(e)
FMC SELECTED
(f)
SYSTEM OK
(g)
SOFTWARE VERSION IS XXX DD-MM-YY
(h)
DATA BASE VERSION IS XXX, DD-MM-YY
(i)
1*XXXXX*
(j)
2*XXXXX*
(k)
3*XXXXX*
NOTE: An all segments LED will precede the status messages.
____ The maintenance labels shown after the database version can be removed by selecting PRESENT STATUS twice when each label shows. The maintenance labels will each be shown for 30 seconds if not removed. The X's indicate "don't care".
(l) END TEST
G. Air/Ground Discrete Test
S 865-119
(1)
Make sure there is a valid glideslope signal from the VOR/ILS Navigation System.
S 745-038
(2)
Set the switch on the GPWC front panel to the PRESENT STATUS position.
(a) Make sure the status message 1*XXX2X* shows after the database version.
S 865-039
(3) Open the AIR/GND RELAY circuit breaker on the P6-3 panel.
(a) Make sure the display changes to 1*XXX3X.
S 865-040
(4) Close the AIR/GND RELAY circuit breaker on the P6-3 panel.
H. BEJ 061-062, 101-112; Flap Discrete Test
S 745-042
(1) Set the switch on the GPWC front panel to the PRESENT STATUS position.
(a) Make sure the status message 1*X1XXX shows after the database version.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH -208 AND ON GPWC ú
34-42-02
ú ú 06 Page 506 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 865-043
WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL
_______ SURFACES WHEN HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS AND STABILIZER ARE FULLY POWERED SURFACES. INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS SUPPLIED.
(2) Set the flaps to 25 degrees.
(a) Make sure the display changes to 1*X0XXX*.
S 865-044
(3) Set the flaps to 15 degrees.
(a) Make sure the display changes to 1*X1XXX*.
S 865-045
(4) Set the FLAP INHIBIT switch to the INHIBIT position.
(a) Make sure the display changes to 1*X0XXX*.
S 865-046
(5)
Set the FLAP INHIBIT switch to the NORMAL position.
S 865-063
(6)
Depressurize the B hydraulic system.
I. BEJ 063-100, 113-999; Flap Discrete Test
S 745-113
(1) Set the switch on the GPWC front panel to the PRESENT STATUS position.
(a) Make sure the status message 1*X3XXX shows after the database version.
S 865-114
WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL
_______ SURFACES WHEN HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS AND STABILIZER ARE FULLY POWERED SURFACES. INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS SUPPLIED.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH -208 AND ON GPWC ú
34-42-02
ú ú 12 Page 507 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(2) Set the flaps to 25 degrees.
(a) Make sure the display changes to 1*X2XXX*.
S 865-115
(3) Set the flaps to 15 degrees.
(a) Make sure the display changes to 1*X3XXX*.
S 865-116
(4) Set the FLAP INHIBIT switch to the INHIBIT position.
(a) Make sure the display changes to 1*X2XXX*.
S 865-117
(5)
Set the FLAP INHIBIT switch to the NORMAL position.
S 865-118
(6)
Depressurize the B hydraulic system.
J. Gear Discrete Test
S 745-047
(1) Set the switch on the GPWC front panel to the PRESENT STATUS position.
(a) Make sure the status message 1*1XXXX* shows after the database version.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 导航 NAVIGATION 3(128)
